Weight Comparisons of Optimized Stiffened, Unstiffened, and Sandwich Cylindrical Shells
- 1 October 1977
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Aircraft
- Vol. 14 (10) , 1000-1008
- https://doi.org/10.2514/3.58885
Abstract
No abstract availableKeywords
This publication has 5 references indexed in Scilit:
- Evaluation of various analytical models for buckling and vibration of stiffened shells.AIAA Journal, 1973
- Structural synthesis of integrally stiffened cylinders.Journal of Spacecraft and Rockets, 1968
- Structural efficiency of orthotropic cylindrical shells subjected toaxial compression.AIAA Journal, 1966
- Optimum structural design concepts for aerospace vehicles.Journal of Spacecraft and Rockets, 1966
- MINIMUM WEIGHT POTENTIALS FOR STIFFENED PLATES AND SHELLSAIAA Journal, 1963